Armstrong Siddeley Leopard

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Leopard
ASLeopard.JPG
Type Radial engine
National originUnited Kingdom
Manufacturer Armstrong Siddeley
First run 1927

The Armstrong Siddeley Leopard was a British 14-cylinder twin-row air-cooled radial aero engine developed in 1927 by Armstrong Siddeley. It was the most powerful radial engine in the world when introduced. [1]

Contents

Variants

Leopard I
700 hp, medium supercharged. Direct drive propeller.
Leopard II
700 hp, geared epicyclic drive.
Leopard III
800 hp, two-valve cylinder head, direct drive.
Leopard IIIA
800 hp, geared epicyclic drive.

Applications

Specifications (Leopard I)

Data fromLumsden, 2003. [5]

General characteristics

Components

Performance

See also

Comparable engines

Related lists

Related Research Articles

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References

Notes

  1. Smith 1981, p.112.
  2. Single engine version only
  3. Mason 1991, p. 140.
  4. Mason 1991, p. 138.
  5. Lumsden 2003, p.69.

Bibliography

  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN   1-85310-294-6.
  • Mason, Francis K. Hawker Aircraft since 1920 (third ed.). London: Putnam, 1991. ISBN   978-0-8517-7839-6.
  • Smith, Herschel. Aircraft Piston Engines. New York, New York: McGraw-Hill, 1981. ISBN   0-07-058472-9.